As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS624.0 AND STA 15R ON RIGHT SIDE OF FUS DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ONTO REAR PRESSURE BULKHEAD AT FS 624 AND STA 15R ON RT PER REO 601R 53-64-985.